NTSB CAROL · Event
Event FTW95LA290
Registry · N210H
FAA Aircraft Registry record.
Make / Model
CESSNA T210R
Year of manufacture
1986 · 9 years old at event
Engine
CONT MOTOR TSIO-520 SER (300 hp)
Seats / Engines
6 seats · 1 engine
Last airworthiness date
19931104
ADS-B equipped
Yes — Mode-S A1BA31
Registrant of record
FREY FARM LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
THE PILOT'S FAILURE TO MAINTAIN AIRSPEED AND THE RESULTING INADVERTENT STALL/MUSH.
Factual narrative
On July 10, 1995, at 1704 central daylight time, a WSK PZL Mielec M-18 Dromader, N210H, collided with machinery during takeoff near De Witt, Arkansas. The commercial pilot was not injured and the airplane sustained substantial damage. No flight plan was filed for the aerial application flight conducted by Bullock Flying Service under Title 14 CFR Part 137. Visual meteorological conditions prevailed for the flight which was originating when the accident occurred. According to the pilot, after a "normal" liftoff, he "started to turn toward field, [and the] aircraft settled." Subsequently, the airplane's left main landing gear "struck [a] barrel and power unit" at the end of the 2,600 foot airstrip. The pilot reported the airplane then "turned sideways knocking out other gear" and came to rest "100 yards from end of runway." Both main landing gear were torn from the airplane and the fuselage and horizontal stabilizer were deformed. The operator reported the airplane was loaded with approximately 3,000 pounds of dry fertilizer. Based on a temperature of 94 degrees and a pressure altitude of 1,000 feet, the density altitude was calculated at 3,500 feet. Using this data, a review of the performance charts in the aircraft flight manual indicated the airplane was within the prescribed limit for gross weight and required a takeoff ground roll distance of 750 feet. There were no reports of any engine or airframe discrepancies. FOLLOWING A 'NORMAL' LIFTOFF, THE PILOT 'STARTED TO TURN TOWARD FIELD, AIRCRAFT SETTLED' AND COLLIDED WITH MACHINERY AT THE END OF THE 2,600 FOOT AIRSTRIP. A REVIEW OF AIRCRAFT PERFORMANCE DATA INDICATED THE AIRPLANE WAS NOT OVER GROSS WEIGHT AND ATMOSPHERIC CONDITIONS REQUIRED A TAKEOFF GROUND ROLL DISTANCE OF 750 FEET. NO ENGINE OR AIRFRAME DISCREPANCIES WERE REPORTED. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1995_FTW95LA290.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Beyond the agency record
Search this event elsewhere.
Pre-filled searches into the sources where news + community discussion of aviation events lives. External sources are reported, not agency. Treat them as signal that something happened, not as fact about what happened.
Entity-clustered aviation events in the press — last 24 hr + 30-day archive.
Official agency record + docket.
Investigative docket: factual reports, photos, transcripts.
Long-running aviation incident database (Flight Safety Foundation).
Community NTSB synthesis blog — often has photos and witness reports.
Gold-standard aviation incident blog.
Aviation industry news search.
GA pilot forum — informed but rumor-prone.
GA pilot subreddit search.
Tail-number page — flight history (free tier limited).
AOPA Air Safety Institute search.
Mainstream press coverage. Recent events only.
Privacy-preserving news search.
External links open in a new tab. We don't ingest their content; we deep-link search queries.
Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type or causal vocabulary (stall). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- NASA NTRS 2026 · Conference Paper
Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
This study presents a computational investigation of steady state aerodynamics of the Subsonic Ultra-Green Aircraft Research (SUGAR) Transonic Truss-Braced Wing (TTBW) configuration over a wide range …
- arXiv 2023 · arXiv preprint
Automating Bird Diverter Installation through Multi-Aerial Robots and Signal Temporal Logic Specifications
This paper tackles the task assignment and trajectory generation problem for bird diverter installation using a fleet of multi-rotors.
- arXiv 2023 · arXiv preprint
Variation of Critical Crystallization Pressure for the Formation of Square Ice in Graphene Nanocapillaries
Two-dimensional square ice in graphene nanocapillaries at room temperature is a fascinating phenomenon and has been confirmed experimentally.
- arXiv 2023 · arXiv preprint
Polycrystallinity enhances stress build-up around ice
Damage caused by freezing wet, porous materials is a widespread problem, but is hard to predict or control. Here, we show that polycrystallinity makes a great difference to the stress build-up process…
- arXiv 2022 · arXiv preprint
Enhanced Prediction of Three-dimensional Finite Iced Wing Separated Flow Near Stall
Icing on three-dimensional wings causes severe flow separation near stall. Standard improved delayed detached eddy simulation (IDDES) is unable to correctly predict the separating reattaching flow due…
- Embry-Riddle Scholarly Commons 2021 · Journal article (JAAER)
Analysis on the Negative Emotional, Physiological, and Cognitive Responses Elicited from of the Activation of a Stall Alarm
Failing to identify an aerodynamic stall can lead to the inability of an aircraft to sustain flight. To warn pilots of an impending or fully-developed stall, many aircraft have safety devices installe…
Browse the full corpus — academia portal ↗